Airfoil: SD8020 Builder: R. Wagner/R. Olsen Comment: clean Number of Reynolds #'s: 8 Average Reynolds #: 30500 Number of angles of attack: 97 alpha / Cl / Cm -6.72 -0.627 0.0000 -5.98 -0.598 0.0000 -5.60 -0.560 0.0000 -5.09 -0.518 0.0000 -4.59 -0.482 0.0000 -4.03 -0.423 0.0000 -3.62 -0.365 0.0000 -3.01 -0.226 0.0000 -2.56 -0.161 0.0000 -1.95 -0.106 0.0000 -1.52 -0.076 0.0000 -0.95 -0.051 0.0000 -0.55 -0.035 0.0000 0.08 -0.013 0.0000 0.49 -0.006 0.0000 1.04 0.018 0.0000 1.47 0.036 0.0000 1.97 0.073 0.0000 2.49 0.124 0.0000 2.98 0.220 0.0000 3.54 0.339 0.0000 3.97 0.393 0.0000 4.57 0.447 0.0000 4.98 0.482 0.0000 5.60 0.505 0.0000 6.06 0.549 0.0000 6.64 0.573 0.0000 7.16 0.606 0.0000 7.65 0.633 0.0000 8.23 0.686 0.0000 8.69 0.702 0.0000 9.12 0.734 0.0000 9.67 0.754 0.0000 10.18 0.717 0.0000 10.66 0.751 0.0000 11.09 0.724 0.0000 11.68 0.725 0.0000 12.18 0.725 0.0000 12.68 0.705 0.0000 13.16 0.710 0.0000 13.68 0.712 0.0000 14.27 0.701 0.0000 14.65 0.721 0.0000 15.27 0.718 0.0000 15.71 0.753 0.0000 16.21 0.775 0.0000 16.70 0.795 0.0000 17.28 0.806 0.0000 17.70 0.862 0.0000 17.25 0.781 0.0000 16.83 0.779 0.0000 16.40 0.774 0.0000 15.77 0.743 0.0000 15.25 0.722 0.0000 14.80 0.725 0.0000 14.33 0.719 0.0000 13.78 0.728 0.0000 13.40 0.706 0.0000 12.76 0.708 0.0000 12.35 0.701 0.0000 11.75 0.671 0.0000 11.38 0.665 0.0000 10.80 0.740 0.0000 10.30 0.747 0.0000 9.81 0.751 0.0000 9.38 0.745 0.0000 8.80 0.763 0.0000 8.39 0.743 0.0000 7.80 0.732 0.0000 7.23 0.698 0.0000 6.83 0.676 0.0000 6.37 0.638 0.0000 5.75 0.607 0.0000 5.35 0.571 0.0000 4.73 0.545 0.0000 4.23 0.499 0.0000 3.73 0.450 0.0000 3.28 0.356 0.0000 2.68 0.239 0.0000 2.20 0.159 0.0000 1.66 0.119 0.0000 1.25 0.082 0.0000 0.61 0.068 0.0000 0.25 0.043 0.0000 -0.41 0.033 0.0000 -0.79 -0.003 0.0000 -1.48 -0.026 0.0000 -1.93 -0.066 0.0000 -2.44 -0.090 0.0000 -2.87 -0.147 0.0000 -3.49 -0.317 0.0000 -3.91 -0.407 0.0000 -4.54 -0.453 0.0000 -5.01 -0.490 0.0000 -5.54 -0.525 0.0000 -6.03 -0.586 0.0000 -6.57 -0.628 0.0000 Tabulated from data in file MS00262.DAT & reduced using program Q01.00L Average Reynolds #: 39100 Number of angles of attack: 97 alpha / Cl / Cm -6.70 -0.644 0.0000 -6.14 -0.601 0.0000 -5.64 -0.564 0.0000 -5.18 -0.525 0.0000 -4.63 -0.482 0.0000 -4.11 -0.445 0.0000 -3.63 -0.404 0.0000 -3.07 -0.324 0.0000 -2.57 -0.190 0.0000 -2.00 -0.091 0.0000 -1.58 -0.063 0.0000 -1.06 -0.023 0.0000 -0.53 -0.002 0.0000 0.00 0.013 0.0000 0.43 0.016 0.0000 0.95 0.033 0.0000 1.47 0.065 0.0000 1.98 0.125 0.0000 2.53 0.257 0.0000 3.05 0.355 0.0000 3.56 0.401 0.0000 4.12 0.444 0.0000 4.60 0.474 0.0000 5.09 0.513 0.0000 5.63 0.553 0.0000 6.11 0.592 0.0000 6.64 0.626 0.0000 7.11 0.666 0.0000 7.60 0.695 0.0000 8.20 0.741 0.0000 8.69 0.766 0.0000 9.15 0.792 0.0000 9.68 0.797 0.0000 10.15 0.787 0.0000 10.64 0.782 0.0000 11.17 0.766 0.0000 11.64 0.735 0.0000 12.15 0.729 0.0000 12.63 0.732 0.0000 13.18 0.743 0.0000 13.69 0.755 0.0000 14.23 0.752 0.0000 14.67 0.786 0.0000 15.20 0.772 0.0000 15.67 0.816 0.0000 16.24 0.847 0.0000 16.70 0.832 0.0000 17.27 0.879 0.0000 17.73 0.879 0.0000 17.32 0.868 0.0000 16.75 0.878 0.0000 16.27 0.854 0.0000 15.77 0.839 0.0000 15.28 0.832 0.0000 14.76 0.851 0.0000 14.32 0.836 0.0000 13.77 0.807 0.0000 13.30 0.804 0.0000 12.77 0.797 0.0000 12.38 0.788 0.0000 11.77 0.793 0.0000 11.31 0.841 0.0000 10.76 0.793 0.0000 10.31 0.795 0.0000 9.75 0.782 0.0000 9.35 0.794 0.0000 8.73 0.765 0.0000 8.34 0.728 0.0000 7.75 0.704 0.0000 7.26 0.666 0.0000 6.73 0.638 0.0000 6.35 0.604 0.0000 5.76 0.564 0.0000 5.27 0.525 0.0000 4.73 0.493 0.0000 4.25 0.443 0.0000 3.67 0.375 0.0000 3.19 0.303 0.0000 2.62 0.231 0.0000 2.18 0.180 0.0000 1.58 0.119 0.0000 1.16 0.072 0.0000 0.58 0.047 0.0000 0.16 0.020 0.0000 -0.44 -0.003 0.0000 -0.89 -0.041 0.0000 -1.47 -0.071 0.0000 -1.88 -0.113 0.0000 -2.52 -0.185 0.0000 -2.97 -0.271 0.0000 -3.57 -0.356 0.0000 -3.98 -0.411 0.0000 -4.62 -0.481 0.0000 -5.01 -0.523 0.0000 -5.61 -0.566 0.0000 -6.06 -0.602 0.0000 -6.62 -0.638 0.0000 Tabulated from data in file MS00259.DAT & reduced using program Q01.00L Average Reynolds #: 52400 Number of angles of attack: 97 alpha / Cl / Cm -6.51 -0.600 0.0000 -6.00 -0.575 0.0000 -5.62 -0.543 0.0000 -5.09 -0.505 0.0000 -4.60 -0.459 0.0000 -4.08 -0.384 0.0000 -3.57 -0.338 0.0000 -3.02 -0.281 0.0000 -2.60 -0.230 0.0000 -1.97 -0.113 0.0000 -1.53 -0.058 0.0000 -0.92 -0.011 0.0000 -0.56 -0.002 0.0000 0.05 0.015 0.0000 0.47 0.031 0.0000 1.00 0.066 0.0000 1.52 0.124 0.0000 2.02 0.197 0.0000 2.56 0.262 0.0000 3.10 0.329 0.0000 3.54 0.372 0.0000 4.23 0.439 0.0000 4.58 0.465 0.0000 5.19 0.514 0.0000 5.62 0.552 0.0000 6.18 0.598 0.0000 6.61 0.627 0.0000 7.14 0.667 0.0000 7.65 0.697 0.0000 8.16 0.733 0.0000 8.68 0.760 0.0000 9.11 0.788 0.0000 9.69 0.793 0.0000 10.23 0.785 0.0000 10.68 0.788 0.0000 11.22 0.814 0.0000 11.71 0.810 0.0000 12.21 0.803 0.0000 12.69 0.803 0.0000 13.22 0.805 0.0000 13.69 0.805 0.0000 14.20 0.796 0.0000 14.67 0.838 0.0000 15.29 0.833 0.0000 15.68 0.849 0.0000 16.35 0.906 0.0000 16.69 0.844 0.0000 17.27 0.872 0.0000 17.73 0.919 0.0000 17.43 0.879 0.0000 16.83 0.892 0.0000 16.40 0.809 0.0000 15.82 0.875 0.0000 15.30 0.812 0.0000 14.83 0.850 0.0000 14.40 0.825 0.0000 13.83 0.814 0.0000 13.41 0.832 0.0000 12.84 0.789 0.0000 12.37 0.785 0.0000 11.79 0.787 0.0000 11.30 0.810 0.0000 10.83 0.844 0.0000 10.40 0.857 0.0000 9.84 0.848 0.0000 9.45 0.845 0.0000 8.81 0.813 0.0000 8.26 0.778 0.0000 7.83 0.745 0.0000 7.38 0.718 0.0000 6.82 0.685 0.0000 6.34 0.650 0.0000 5.76 0.606 0.0000 5.20 0.563 0.0000 4.68 0.523 0.0000 4.22 0.487 0.0000 3.71 0.453 0.0000 3.29 0.411 0.0000 2.71 0.358 0.0000 2.27 0.301 0.0000 1.65 0.199 0.0000 1.26 0.122 0.0000 0.62 0.099 0.0000 0.24 0.093 0.0000 -0.39 0.081 0.0000 -0.83 0.058 0.0000 -1.44 0.003 0.0000 -1.81 -0.056 0.0000 -2.48 -0.172 0.0000 -2.88 -0.222 0.0000 -3.53 -0.285 0.0000 -3.93 -0.344 0.0000 -4.53 -0.389 0.0000 -5.04 -0.431 0.0000 -5.55 -0.468 0.0000 -6.01 -0.509 0.0000 -6.61 -0.555 0.0000 Tabulated from data in file MS00260.DAT & reduced using program Q01.00L Average Reynolds #: 60600 Number of angles of attack: 97 alpha / Cl / Cm -6.69 -0.681 0.0000 -6.13 -0.645 0.0000 -5.66 -0.609 0.0000 -5.02 -0.561 0.0000 -4.63 -0.529 0.0000 -4.15 -0.486 0.0000 -3.66 -0.436 0.0000 -3.03 -0.373 0.0000 -2.60 -0.319 0.0000 -2.01 -0.230 0.0000 -1.61 -0.146 0.0000 -1.04 -0.079 0.0000 -0.56 -0.056 0.0000 0.05 -0.036 0.0000 0.44 -0.032 0.0000 1.02 0.005 0.0000 1.43 0.073 0.0000 2.10 0.182 0.0000 2.54 0.238 0.0000 3.07 0.289 0.0000 3.56 0.325 0.0000 4.03 0.367 0.0000 4.55 0.405 0.0000 5.13 0.455 0.0000 5.57 0.493 0.0000 6.14 0.539 0.0000 6.63 0.574 0.0000 7.10 0.606 0.0000 7.60 0.640 0.0000 8.10 0.677 0.0000 8.61 0.708 0.0000 9.17 0.738 0.0000 9.67 0.754 0.0000 10.17 0.752 0.0000 10.68 0.766 0.0000 11.22 0.769 0.0000 11.66 0.742 0.0000 12.21 0.744 0.0000 12.67 0.713 0.0000 13.23 0.733 0.0000 13.69 0.772 0.0000 14.27 0.761 0.0000 14.70 0.778 0.0000 15.20 0.837 0.0000 15.64 0.767 0.0000 16.22 0.799 0.0000 16.68 0.829 0.0000 17.25 0.851 0.0000 17.70 0.823 0.0000 17.34 0.855 0.0000 16.73 0.850 0.0000 16.31 0.796 0.0000 15.78 0.818 0.0000 15.31 0.790 0.0000 14.77 0.796 0.0000 14.28 0.765 0.0000 13.75 0.715 0.0000 13.30 0.751 0.0000 12.75 0.730 0.0000 12.23 0.734 0.0000 11.73 0.767 0.0000 11.30 0.772 0.0000 10.76 0.790 0.0000 10.31 0.779 0.0000 9.75 0.762 0.0000 9.33 0.759 0.0000 8.75 0.735 0.0000 8.28 0.706 0.0000 7.75 0.671 0.0000 7.31 0.639 0.0000 6.70 0.595 0.0000 6.32 0.565 0.0000 5.72 0.519 0.0000 5.23 0.480 0.0000 4.68 0.437 0.0000 4.25 0.400 0.0000 3.65 0.352 0.0000 3.22 0.304 0.0000 2.60 0.243 0.0000 2.18 0.194 0.0000 1.57 0.099 0.0000 1.13 0.002 0.0000 0.53 -0.025 0.0000 0.12 -0.025 0.0000 -0.47 -0.044 0.0000 -0.96 -0.083 0.0000 -1.50 -0.144 0.0000 -1.98 -0.230 0.0000 -2.57 -0.326 0.0000 -2.96 -0.363 0.0000 -3.60 -0.422 0.0000 -4.01 -0.468 0.0000 -4.63 -0.516 0.0000 -5.07 -0.557 0.0000 -5.67 -0.606 0.0000 -6.14 -0.644 0.0000 -6.68 -0.685 0.0000 Tabulated from data in file MS00261.DAT & reduced using program Q01.00L Average Reynolds #: 81100 Number of angles of attack: 97 alpha / Cl / Cm -6.53 -0.641 0.0000 -6.15 -0.621 0.0000 -5.68 -0.583 0.0000 -5.06 -0.529 0.0000 -4.62 -0.494 0.0000 -4.13 -0.458 0.0000 -3.62 -0.409 0.0000 -3.09 -0.355 0.0000 -2.61 -0.317 0.0000 -2.10 -0.234 0.0000 -1.58 -0.161 0.0000 -0.97 -0.049 0.0000 -0.57 -0.014 0.0000 -0.05 -0.001 0.0000 0.45 0.005 0.0000 0.99 0.067 0.0000 1.48 0.142 0.0000 2.09 0.223 0.0000 2.53 0.271 0.0000 3.02 0.305 0.0000 3.57 0.352 0.0000 4.02 0.397 0.0000 4.55 0.440 0.0000 5.11 0.484 0.0000 5.56 0.518 0.0000 6.14 0.564 0.0000 6.64 0.600 0.0000 7.22 0.642 0.0000 7.62 0.670 0.0000 8.12 0.703 0.0000 8.64 0.736 0.0000 9.14 0.763 0.0000 9.63 0.786 0.0000 10.20 0.801 0.0000 10.63 0.785 0.0000 11.17 0.794 0.0000 11.67 0.735 0.0000 12.15 0.763 0.0000 12.66 0.748 0.0000 13.19 0.724 0.0000 13.68 0.740 0.0000 14.18 0.728 0.0000 14.68 0.750 0.0000 15.28 0.825 0.0000 15.70 0.804 0.0000 16.22 0.829 0.0000 16.67 0.837 0.0000 17.27 0.824 0.0000 17.64 0.826 0.0000 17.31 0.836 0.0000 16.75 0.818 0.0000 16.35 0.814 0.0000 15.82 0.803 0.0000 15.31 0.820 0.0000 14.75 0.797 0.0000 14.30 0.764 0.0000 13.74 0.730 0.0000 13.33 0.737 0.0000 12.74 0.752 0.0000 12.28 0.768 0.0000 11.78 0.777 0.0000 11.34 0.766 0.0000 10.77 0.782 0.0000 10.34 0.785 0.0000 9.77 0.789 0.0000 9.39 0.776 0.0000 8.76 0.748 0.0000 8.28 0.721 0.0000 7.77 0.687 0.0000 7.33 0.653 0.0000 6.71 0.612 0.0000 6.27 0.574 0.0000 5.70 0.531 0.0000 5.25 0.494 0.0000 4.70 0.451 0.0000 4.28 0.414 0.0000 3.65 0.365 0.0000 3.25 0.327 0.0000 2.63 0.277 0.0000 2.13 0.232 0.0000 1.61 0.157 0.0000 1.15 0.084 0.0000 0.57 -0.008 0.0000 0.16 -0.008 0.0000 -0.46 -0.019 0.0000 -0.86 -0.044 0.0000 -1.51 -0.156 0.0000 -1.90 -0.228 0.0000 -2.53 -0.301 0.0000 -2.99 -0.334 0.0000 -3.57 -0.402 0.0000 -3.97 -0.434 0.0000 -4.60 -0.487 0.0000 -5.11 -0.526 0.0000 -5.62 -0.567 0.0000 -6.05 -0.606 0.0000 -6.64 -0.651 0.0000 Tabulated from data in file MS00263.DAT & reduced using program Q01.00L Average Reynolds #: 101800 Number of angles of attack: 97 alpha / Cl / Cm -6.56 -0.623 0.0000 -6.03 -0.586 0.0000 -5.66 -0.557 0.0000 -5.07 -0.506 0.0000 -4.61 -0.465 0.0000 -4.05 -0.420 0.0000 -3.57 -0.382 0.0000 -3.03 -0.318 0.0000 -2.59 -0.277 0.0000 -2.01 -0.218 0.0000 -1.57 -0.161 0.0000 -0.97 -0.059 0.0000 -0.52 0.015 0.0000 0.09 0.036 0.0000 0.46 0.038 0.0000 1.13 0.146 0.0000 1.55 0.204 0.0000 2.11 0.260 0.0000 2.56 0.288 0.0000 3.07 0.343 0.0000 3.55 0.381 0.0000 4.09 0.426 0.0000 4.60 0.469 0.0000 5.10 0.512 0.0000 5.64 0.559 0.0000 6.19 0.604 0.0000 6.65 0.635 0.0000 7.17 0.674 0.0000 7.67 0.709 0.0000 8.16 0.741 0.0000 8.74 0.778 0.0000 9.14 0.797 0.0000 9.69 0.823 0.0000 10.10 0.812 0.0000 10.73 0.780 0.0000 11.19 0.788 0.0000 11.67 0.779 0.0000 12.24 0.729 0.0000 12.68 0.743 0.0000 13.27 0.748 0.0000 13.69 0.737 0.0000 14.22 0.759 0.0000 14.68 0.793 0.0000 15.30 0.813 0.0000 15.69 0.816 0.0000 16.37 0.854 0.0000 16.66 0.833 0.0000 17.25 0.837 0.0000 17.70 0.886 0.0000 17.27 0.840 0.0000 16.75 0.866 0.0000 16.41 0.801 0.0000 15.79 0.809 0.0000 15.27 0.775 0.0000 14.82 0.764 0.0000 14.38 0.761 0.0000 13.80 0.748 0.0000 13.36 0.740 0.0000 12.81 0.741 0.0000 12.38 0.742 0.0000 11.70 0.763 0.0000 11.28 0.761 0.0000 10.85 0.799 0.0000 10.40 0.794 0.0000 9.81 0.814 0.0000 9.36 0.798 0.0000 8.78 0.768 0.0000 8.38 0.743 0.0000 7.78 0.703 0.0000 7.27 0.665 0.0000 6.78 0.629 0.0000 6.33 0.596 0.0000 5.70 0.549 0.0000 5.33 0.517 0.0000 4.72 0.465 0.0000 4.32 0.432 0.0000 3.67 0.377 0.0000 3.30 0.347 0.0000 2.65 0.294 0.0000 2.25 0.254 0.0000 1.67 0.207 0.0000 1.27 0.150 0.0000 0.61 0.039 0.0000 0.22 0.008 0.0000 -0.41 0.009 0.0000 -0.80 -0.036 0.0000 -1.42 -0.144 0.0000 -1.82 -0.197 0.0000 -2.48 -0.257 0.0000 -2.90 -0.295 0.0000 -3.54 -0.364 0.0000 -4.04 -0.407 0.0000 -4.55 -0.451 0.0000 -5.06 -0.495 0.0000 -5.56 -0.541 0.0000 -6.00 -0.578 0.0000 -6.57 -0.620 0.0000 Tabulated from data in file MS00264.DAT & reduced using program Q01.00L Average Reynolds #: 204200 Number of angles of attack: 33 alpha / Cl / Cm -6.54 -0.637 0.0000 -5.02 -0.504 0.0000 -3.46 -0.364 0.0000 -1.67 -0.211 0.0000 -0.35 -0.036 0.0000 1.15 0.147 0.0000 2.63 0.292 0.0000 4.27 0.437 0.0000 5.75 0.565 0.0000 7.27 0.692 0.0000 8.86 0.807 0.0000 10.13 0.855 0.0000 11.86 0.833 0.0000 13.51 0.800 0.0000 14.93 0.760 0.0000 16.36 0.772 0.0000 17.84 0.788 0.0000 15.93 0.771 0.0000 14.53 0.750 0.0000 12.93 0.795 0.0000 11.63 0.840 0.0000 10.26 0.860 0.0000 8.71 0.790 0.0000 7.19 0.680 0.0000 5.69 0.558 0.0000 4.09 0.416 0.0000 2.58 0.282 0.0000 0.94 0.109 0.0000 -0.47 -0.058 0.0000 -2.08 -0.256 0.0000 -3.58 -0.384 0.0000 -5.20 -0.531 0.0000 -6.70 -0.656 0.0000 Tabulated from data in file JG00255.DAT & reduced using program Q01.00L Average Reynolds #: 305600 Number of angles of attack: 33 alpha / Cl / Cm -6.79 -0.660 0.0000 -4.82 -0.491 0.0000 -3.24 -0.346 0.0000 -1.79 -0.196 0.0000 -0.25 -0.028 0.0000 1.21 0.112 0.0000 2.65 0.286 0.0000 4.15 0.426 0.0000 5.65 0.560 0.0000 7.23 0.691 0.0000 8.83 0.812 0.0000 10.21 0.882 0.0000 11.61 0.861 0.0000 13.16 0.798 0.0000 14.66 0.777 0.0000 16.10 0.797 0.0000 17.78 0.810 0.0000 15.87 0.781 0.0000 14.46 0.761 0.0000 12.81 0.818 0.0000 11.49 0.855 0.0000 10.24 0.875 0.0000 8.72 0.803 0.0000 7.17 0.684 0.0000 5.64 0.553 0.0000 4.08 0.412 0.0000 2.58 0.275 0.0000 1.06 0.091 0.0000 -0.52 -0.054 0.0000 -2.07 -0.235 0.0000 -3.57 -0.377 0.0000 -5.19 -0.526 0.0000 -6.70 -0.656 0.0000 Tabulated from data in file JG00257.DAT & reduced using program Q01.00L File sd8020.lft created on 12-05-1997 at 15:25:52 using program FORMAT